中高碳贝氏体钢的组织和耐磨性

对一种新型中高碳贝氏体钢的组织，转为动力学和耐磨性进行了研究，中高碳贝氏体钢空冷后的组织为贝氏体，马氏体，碳化物和残留奥氏体，组织细小均匀，大截面实物硬度测定和组织观察表明，截面上具有高硬度，并组织分布均匀，中高碳贝氏体钢具有高的耐磨性。     

激光功率对Fe基复合熔覆层中TiC形态及性能的影响

采用激光熔覆技术在高锰钢基材上制备了不同激光功率下的Fe基复合熔覆层,研究了不同激光功率对熔覆层中Ti C形态及性能的影响。试验结果表明,熔覆层组分包含奥氏体和TiC,随着激光功率的增加,TiC析出相由单一颗粒状转变为梅花状、蕨状及颗粒状的组合,晶粒尺寸增加,熔覆层硬度和耐磨性逐步提升。     

前驱体碳化粉末反应火焰喷涂制备TiC增强金属复合涂层

采用前驱体碳化复合技术制备了Ti-Fe-C和Ti-Ni-C两种体系的反应热喷涂复合粉末,通过氧乙炔火焰喷涂原位合成并沉积了TiC增强Fe基和Ni基复合涂层.利用XRD、SEM和EDS研究了复合粉末、涂层的相组成和组织结构,考察了TiC/Fe、TiC/Ni复合涂层的硬度和耐磨性.结果表明: 复合粉末在喷涂过程中反应充分,可分别生成以Fe和Ni为粘结相的TiC增强涂层;两种涂层都是由TiC颗粒均匀分布的复合强化片层和TiC聚集片层叠加而成,TiC/Fe复合涂层的片层较薄,而TiC/Ni涂层中TiC的聚集片层较少;TiC/Fe涂层的硬度高于TiC/Ni涂层,两者的耐磨性能分别约为Ni60涂层的11倍和6倍.     

燃烧合成/准热等静压TiC-Fe基复合材料耐磨损性能的研究

利用燃烧合成结合准热等静压技术(SHS/PHIP)原位合成了TiC颗粒增强铁基复合材料。利用SEM,XRD研究了复合材料的相组成和显微组织。结果表明:该复合材料由TiC增强颗粒和金属Fe粘结相组成,组织较为致密,球形的TiC颗粒相被包围在近于立体网状结构的Fe粘结相中。TiC颗粒相和金属Fe粘结相的界面结合良好。在橡胶轮式磨损试验条件下,TiC颗粒增强铁基复合材料表现出良好的耐磨性能。其磨损机制主要是磨粒磨损和少量硬质相脱落。     

热处理工艺对Cr12MoV钢组织、硬度及耐磨性的影响

本试验研究了不同淬火和回火工艺热处理对Cr12MoV钢组织、硬度和磨损性能的影响。实验结果表明:当在1050~1100℃范围内淬火、520℃回火时,得隐针马氏体+少量残余奥氏体组织,材料硬度与耐磨性均较好;当在1100℃淬火,各温度二次回火硬度均较一次回火高,当在550℃回火时,试验钢实现二次硬化,且残余奥氏体大量转变,硬度和耐磨性达最大值,材料性能最优。     

高钛钢中TiC析出机制

通过凝固实验并结合Thermo-Calc软件研究了高钛钢(Ti 质量分数为0.6％)在凝固过程中 TiC 的析出方式及形态.结果表明：由于选分结晶的作用,TiC在凝固最后阶段沿着原始奥氏体晶界析出,并形成离异共晶组织,以片状或杆状形式存在,析出相厚度约为1~3μm.Mo 溶入 TiC 后形成(Ti,Mo)C,相分析数据表明,Ti/Mo 质量比为3.4.采用热力学软件及TiC溶解度积分别得出TiC开始析出温度分别为1453及1487℃,析出温度略高于固相线温度,析出质量分数可以达到0.35％.     

TiC含量对激光熔覆TiC增强双相不锈钢复合涂层性能的影响

采用激光熔覆技术在40 Cr Ni Mo基材上制备了TiC增强双相不锈钢复合熔覆层,熔覆层物相主要由奥氏体、马氏体、M₇C₃型碳化物和TiC组成。其中M₇C₃型碳化物主要包括Fe₇C₃、Cr₇C₃或者(Fe、Cr)₇C₃三种,TiC按尺寸可分为熔解后析出的微米级TiC以及粗大的未熔TiC颗粒。析出的TiC颗粒为方块状,随着TiC添加量增加,呈花瓣状长大。未熔TiC颗粒与基材形成了扩散界面,具有很好的界面结合性。当加入30 wt.%TiC时,熔覆层具有最好的耐磨性,硬度可达55.26 HRC,磨损体积为2.54×10^-2 mm³,耐磨性是基材的3.37倍。     

TiC含量对激光熔覆Fe基复合涂层组分和性能的影响

采用激光熔覆技术在高锰钢基材上制备了不同TiC含量的Fe基复合涂层,研究了TiC含量对熔覆层组分和性能的影响.试验结果表明,熔覆层化学组分包含奥氏体、M7C3碳化物、TiC析出相和未熔TiC颗粒.随着TiC含量的增加,熔覆层硬度逐步增加,耐磨性能先增加后降低.     

Microstructure and Wear Resistance in Medium and High C Steels Treated by Quenching and Partitioning

The quenching and partitioning (Q&P) steels have shown to be promising candidates to be applied in fields where wear resistance is required. In this study, a medium and a high C steel are heat treated by Q&P and the resulting microstructure, hardness, and wear resistance are characterized. The mechanical stability of the austenite phase under wear test conditions is investigated. It is found that the stability of austenite is very high in the high C steel and decreases in the medium C steel. Additionally, the hardness and wear behavior of the Q&P-treated steels are compared with the results obtained for quenching and tempering (Q&T) treated samples, showing that, although the hardness of Q&P steels is quite lower, the obtained wear rates are similar. It means that in the studied Q&P steels, although the austenite transformation into martensite does not occur considerably, the presence of austenite might play a key role in the wear resistance.     

Correlation of microstructure and abrasive and sliding wear resistance of (TiC,SiC)/Ti-6Al-4V surface composites fabricated by high-energy electron-beam irradiation

This study is concerned with the correlation of microstructure and abrasive and sliding wear resistance of (TiC,SiC)/Ti-6Al-4V surface composites fabricated by high-energy electron-beam irradiation. The mixtures of TiC, SiC, Ti + SiC, or TiC+SiC powders and CaF₂ flux were deposited on a Ti-6Al-4V substrate, and then an electron beam was irradiated on these mixtures. The surface composite layers of 1.2 to 2.1 mm in thickness were homogeneously formed without defects and contained a large amount (30 to 66 vol pct) of hard precipitates such as TiC and Ti₅Si₃ in the martensitic matrix. This microstructural modification, including the formation of hard precipitates in the surface composite layer, improved the hardness and abrasive wear resistance. Particularly in the surface composite fabricated with TiC + SiC powders, the abrasive wear resistance was greatly enhanced to a level 25 times higher than that of the Ti alloy substrate because of the precipitation of 66 vol pct of TiC and Ti₅Si₃ in the hardened martensitic matrix. During the sliding wear process, hard and coarse TiC and Ti₅Si₃ precipitates fell off from the matrix, and their wear debris worked as abrasive particles, thereby reducing the sliding wear resistance. On the other hand, needle-shaped Ti₅Si₃ particles, which did not play a significant role in enhancing abrasive wear resistance, lowered the friction coefficient and, accordingly, decelerated the sliding wear, because they played more of the role of solid lubricants than as abrasive particles after they fell off from the matrix. These findings indicated that high-energy electron-beam irradiation was useful for the development of Ti-based surface composites with improved abrasive and sliding wear resistance, although the abrasive and sliding-wear data should be interpreted by different wear mechanisms.     

Improvement of hardness and wear resistance of (TiC,TiB)/Ti-6Al-4V surface-alloyed materials fabricated by high-energy electron-beam irradiation

The objective of this study is to investigate microstructure, hardness, and wear properties of three kinds of (TiC,TiB)/Ti-6Al-4V surface-alloyed materials fabricated by high-energy electron-beam irradiation. The mixtures of Ti+C, TiC+TiB₂, and Ti+B₄C powders and CaF₂ flux were deposited on a Ti-6A1-4V substrate, and then high-energy electron beam was irradiated on these mixtures. The surface-alloyed layers of 0.9 to 1.6 mm in thickness were homogeneously formed, and contained a large amount (30 to 44 vol. pct) of hard precipitates such as TiC and TiB in the martensitic matrix. This microstructural modification improved the hardness and wear resistance of the surface-alloyed layer 2 times and 6 to 9 times, respectively, greater than that of the substrate. Particularly, the surface-alloyed material fabricated with Ti+B₄C powders had a larger volume fraction of TiB and TiC homogeneously distributed in the martensitic matrix, and thus showed the best hardness and wear resistance. These findings suggested that the surface-alloying using high-energy electron-beam irradiation was economical and useful for the development of titanium-base surface-alloyed materials with improved hardness and wear properties.     

含钛中锰钢淬火-配分组织及力学性能

为了研究淬火配分含钛中锰钢的组织与力学性能,借助扫描电子显微镜,透射电子显微镜、电子背散射衍射技术与万能拉伸试验机、磨粒磨损试验机等,分析与测试了含钛中锰钢在165～240℃淬火380℃配分处理后组织、强度、塑性与磨粒磨损性能.结果 表明,试验钢淬火-配分组织主要为板条状一次马氏体、块状二次马氏体及残余奥氏体,同时含有...     

热等静压TiC_p/30CrNi4Mo钢基复合材料的组织与性能

采用球磨与热等静压相结合的方法制备TiC_p/30Cr Ni4Mo钢基复合材料,研究材料的显微组织、密度、硬度、常温和高温拉伸性能以及摩擦磨损性能。结果表明,TiC_p/30Cr Ni4Mo钢基复合材料的组织均匀细小,基体组织主要为细片状珠光体、铁素体和少量残余奥氏体,Ti C颗粒弥散分布在基体上,与基体结合牢固;复合材料的相对密度高达99.7%,硬度为49 HRC,抗拉强度高达1 266 MPa,伸长率为4.0%;复合材料具有较好的高温力学性能,400℃时复合材料抗拉强度仍高达1 135 MPa;在200 N载荷条件下,复合材料的耐磨损性能较原30Cr Ni4Mo材料提高约4倍,磨损形式主要表现为轻微的磨粒磨损;复合材料经950℃水淬和520℃回火后,抗拉强度高达1 325 MPa,伸长率为4.6%。     

TiC颗粒增强铜基复合材料的研究

以电解铜粉和TiC粉为原料, 采用粉末冶金法制备了增强体质量分数为5%、10%、15%、20%的TiC颗粒增强铜基复合材料。通过对显微组织的观察和对相对密度、硬度、电导率、磨损率、摩擦系数的测试, 研究了增强相质量分数、烧结温度对复合材料组织性能的影响。研究结果表明, TiC颗粒除少量团聚外均匀分布在基体上, 并与基体结合良好; 随烧结温度升高, 铜基复合材料的密度和硬度均有所增加; 随增强相质量分数的增加, 硬度增加, 相对密度和电导率均有所下降; 磨损率则表现为先降低后有所增加的趋势, 磨损率在TiC质量分数为15%时最低; 铜基复合材料的摩擦系数明显低于纯铜, 其磨损机制主要以磨粒磨损为主。     

TiC含量对Mo_2FeB_2基金属陶瓷的组织与力学性能的影响

在制备Mo_2FeB_2基金属陶瓷原料中,添加3%~12%(质量分数)TiC微粉,经球磨、压制、真空烧结后,采用金相显微镜、扫描电镜和能谱仪分析了试样的显微组织和微区成分,采用硬度计和材料试验机检测其力学性能,并与砂轮对磨分析其耐磨性能。结果表明:添加TiC有助于细化Mo_2FeB_2基金属陶瓷的组织和提高其均匀性,TiC能大幅度提高Mo_2FeB_2基金属陶瓷的硬度、抗弯强度和耐磨性。     

析出粒子对钛微合金化高强钢奥氏体晶粒长大的影响

通过析出粒子与奥氏体晶粒尺寸的定量关系,建立奥氏体晶粒长大模型,计算TiN和TiC析出粒子共同作用下钛微合金化钢奥氏体晶粒尺寸.根据析出相质点理论计算结果表明:随着加热温度的升高,析出粒子体积分数逐渐减少,粒子半径逐渐增大,TiC粒子强烈阻止奥氏体晶粒长大,TiN粒子对奥氏体晶粒长大钉扎效果一般.采用实验测试手段测量不同加热温度下保温30 min后实验钢的奥氏体晶粒尺寸,与理论计算结果吻合较好.      

Comparison of the microstructures and abrasive wear properties of stellite hardfacing alloys deposited by arc welding and laser cladding

The microstructure of cobalt-based hardfacing alloys deposited by manual metal arc (MMA) welding, tungsten inert gas (TIG) welding, and laser cladding has been investigated as part of a study attempting to establish the relationship between microstructure and abrasive wear properties. For typical deposition conditions, the differences in freezing rates associated with the three processes are found to give rise to large differences in microstructure. The MMA process is found to lead to the largest degree of dilution of the hardfacing deposit; the TIG and laser deposits exhibited much lower levels of mixing with the base plate. For the deposition conditions used in this study and for the alloys examined, the scale of the microstructure decreases in the order MMA, TIG, and laser cladding, leading to an increase in the deposit hardness in the same order. It is found that with alumina as an abrasive, the wear rate persistently is higher with the MMA deposits (which have the coarsest microstructure with the lowest starting hardness), the weight loss being approximately linear with time. The laser and TIG deposits, which have more refined microstructures and slightly higher carbon concentrations, both are found to exhibit significantly lower wear rates. Initially, the TIG samples are the most resistant to abrasion, even though their microstructure compares with that of the laser samples; this is a consequence of their higher ductility associated with a lower rate of strain hardening. The laser samples, which contain a lower matrix iron concentration, strain harden more rapidly; consequently, they exhibit an initial decrease in wear rate. With the much harder silicon carbide abrasive, all samples show similar wear rates which do not decrease with time. The wear data are found to correlate with scanning and transmission electron microscopy observations, and it is possible to rationalize the interaction among microstructure, abrasive, and alloy deposition processes.     

A Study on Influence of Aging Treatment on Sliding Wear Resistance of a Nickel Based Hardfacing Alloy

In the present study, Ni-based Colmonoy 5 was deposited on Type 316L (N) stainless steel. The deposit was aged at 580 and 650°C for 5,000 h to study the influence of aging on sliding wear resistance. The aged deposits show more wear loss due to reduced hardness. However, the reduced hardness after aging was not reflected on wear test at 550°C irrespective of sliding distance. This is due to stability of microstructure as well as the generation of oxide layer during high temperature tests. Subsequently, an empirical relation was developed based on outcome experimental data using full factorial design of experiments in terms of hardness (H), test temperature (T) and sliding distance (D). Based on the empirical relation, it was found that the test temperatures (T) play a predominant role on wear loss than hardness (H) and sliding distance (D). Further, the developed relationships were validated using analysis of variance (ANOVA).